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Accuracy Analysis of Ionospheric Delay of Low Earth Orbit Satellites by using NeQuick G Model

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초록

Since the Global Navigation Satellite System (GNSS) signal received from the low Earth orbit (LEO) satellite is only affected by the upper ionosphere, the magnitude of the ionospheric delay of Global Positioning System (GPS) signal received from ground user is different. Therefore, the ground-based two-dimensional ionospheric model cannot be applied to LEO satellites. The NeQuick model used in Galileo provides the ionospheric delay according to the user's altitude, so it can be used in the ionospheric model of the LEO satellites. However, the NeQuick model is not suitable for space receivers because of the high computational cost. A simplified NeQuick model with reduced computing time was recently presented. In this study, the computing time of the NeQuick model and the simplified NeQuick model was analyzed based on the GPS Klobuchar model. The NeQuick and simplified NeQuick model were applied to the GNSS data from GRACE-B, Swarm-C, and GOCE satellites to analyze the performance of the ionospheric correction and positioning. The difference in computing time between the NeQuick and simplified NeQuick model was up to 90%, but the difference in ionospheric accuracy was not as large as within 4.5%.

Abstract

Since the Global Navigation Satellite System (GNSS) signal received from the low Earth orbit (LEO) satellite is only affected by the upper ionosphere, the magnitude of the ionospheric delay of Global Positioning System (GPS) signal received from ground user is different. Therefore, the ground-based two-dimensional ionospheric model cannot be applied to LEO satellites. The NeQuick model used in Galileo provides the ionospheric delay according to the user's altitude, so it can be used in the ionospheric model of the LEO satellites. However, the NeQuick model is not suitable for space receivers because of the high computational cost. A simplified NeQuick model with reduced computing time was recently presented. In this study, the computing time of the NeQuick model and the simplified NeQuick model was analyzed based on the GPS Klobuchar model. The NeQuick and simplified NeQuick model were applied to the GNSS data from GRACE-B, Swarm-C, and GOCE satellites to analyze the performance of the ionospheric correction and positioning. The difference in computing time between the NeQuick and simplified NeQuick model was up to 90%, but the difference in ionospheric accuracy was not as large as within 4.5%.

참고문헌 (13)

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  5. Jeongrae Kim, "NeQuick G model based scale factor determination for using SBAS ionosphere corrections at low earth orbit", Advances in Space Research, 65(5), pp.1414~1423 (2020), Elsevier BV[DOI]
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  7. 김민규, "NeQuick G 모델을 이용한 저궤도위성 전리층 지연의 실시간 변환 계수 결정", 한국항행학회논문지, 22(4), pp.271~278 (2018), 한국항행학회[DOI]
  8. 이창문, "단일주파수 GNSS 수신기용 실시간 전리층 지연 보정 모델 비교 : Klobuchar 모델과 NeQuick 모델", 한국측량학회지, 28(4), pp.413~420 (2010), 한국측량학회
  9. Oliver Montenbruck, "Ionospheric Correction for GPS Tracking of LEO Satellites", Journal of Navigation, 55(2), pp.293~304 (2002), Cambridge University Press (CUP)[DOI]
  10. Oliver Montenbruck, "NeQuick-G performance assessment for space applications", GPS Solutions, 24(1) (2020), Springer Science and Business Media LLC[DOI]
  11. M. Noja, "Long-term analysis of ionospheric polar patches based on CHAMP TEC data", Radio Science, 48(3), pp.289~301 (2013), American Geophysical Union (AGU)[DOI]
  12. S.M. Radicella, "The evolution of the DGR approach to model electron density profiles", Advances in Space Research, 27(1), pp.35~40 (2001), Elsevier BV[DOI]
  13. K. Rawer, "Replacement of the present sub-peak plasma density profile by a unique expression", Advances in Space Research, 2(10), pp.183~190 (1982), Elsevier BV[DOI]

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